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Attitude Control System for InnoSAT

To develop attitude control algorithms software; ACS is the part of the ADCS payload. The ACS has Adaptive Predictive Fuzzy Logic. The objective of this project is to develop attitude control algorithms that are going to be tested when the InnoSAT is in the orbit. Upon deployment in the near Equitor...

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Main Author: Anon
Format: Other
Language:English
Published: Universiti Malaysia Perlis 2009
Subjects:
InnoSAT
Attitude control algorithms
UniMAP > Research and development
Higher education > Research and development
UniMAP > Achievement, Research
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/5514
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id my.unimap-5514
record_format dspace
spelling my.unimap-55142009-04-21T04:26:02Z Attitude Control System for InnoSAT Anon InnoSAT Attitude control algorithms UniMAP -- Research and development Higher education -- Research and development UniMAP -- Achievement, Research To develop attitude control algorithms software; ACS is the part of the ADCS payload. The ACS has Adaptive Predictive Fuzzy Logic. The objective of this project is to develop attitude control algorithms that are going to be tested when the InnoSAT is in the orbit. Upon deployment in the near Equitorial Orbit (NEqO), it will tumble and has difficulty to oriented itself. Hence the needs to control the designated orientation. This is called Attitude Control System (ACS). On receiving the desired and actual angles, intelligent control algorithms using the Adaptive Predective Fuzzy Logic Control (APFLC) and Adaptive Parametric Black Box (APBB) will be employed separately according to the command sequence that will be determined by the InnoSAT's main controller. Resulted data from this control algorithm experiments will be downlink to the ground contro for analysis. 2009-04-21T04:26:02Z 2009-04-21T04:26:02Z 2009 Other http://hdl.handle.net/123456789/5514 en Universiti Malaysia Perlis
institution Universiti Malaysia Perlis
building UniMAP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Perlis
content_source UniMAP Library Digital Repository
url_provider http://dspace.unimap.edu.my/
language English
topic InnoSAT
Attitude control algorithms
UniMAP -- Research and development
Higher education -- Research and development
UniMAP -- Achievement, Research
spellingShingle InnoSAT
Attitude control algorithms
UniMAP -- Research and development
Higher education -- Research and development
UniMAP -- Achievement, Research
Anon
Attitude Control System for InnoSAT
description To develop attitude control algorithms software; ACS is the part of the ADCS payload. The ACS has Adaptive Predictive Fuzzy Logic. The objective of this project is to develop attitude control algorithms that are going to be tested when the InnoSAT is in the orbit. Upon deployment in the near Equitorial Orbit (NEqO), it will tumble and has difficulty to oriented itself. Hence the needs to control the designated orientation. This is called Attitude Control System (ACS). On receiving the desired and actual angles, intelligent control algorithms using the Adaptive Predective Fuzzy Logic Control (APFLC) and Adaptive Parametric Black Box (APBB) will be employed separately according to the command sequence that will be determined by the InnoSAT's main controller. Resulted data from this control algorithm experiments will be downlink to the ground contro for analysis.
format Other
author Anon
author_facet Anon
author_sort Anon
title Attitude Control System for InnoSAT
title_short Attitude Control System for InnoSAT
title_full Attitude Control System for InnoSAT
title_fullStr Attitude Control System for InnoSAT
title_full_unstemmed Attitude Control System for InnoSAT
title_sort attitude control system for innosat
publisher Universiti Malaysia Perlis
publishDate 2009
url http://dspace.unimap.edu.my/xmlui/handle/123456789/5514
_version_ 1643788369844502528
score 13.222552

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